Invention Grant
- Patent Title: Element for distributing a cooling fluid and associated turbine ring assembly
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Application No.: US17737574Application Date: 2022-05-05
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Publication No.: US11753962B2Publication Date: 2023-09-12
- Inventor: Pierre Jean-Baptiste Metge , Sébastien Serge Francis Congratel , Lucien Henri Jacques Quennehen
- Applicant: SAFRAN AIRCRAFT ENGINES
- Applicant Address: FR Paris
- Assignee: SAFRAN AIRCRAFT ENGINES
- Current Assignee: SAFRAN AIRCRAFT ENGINES
- Current Assignee Address: FR Paris
- Agency: Pillsbury Winthrop Shaw Pittman LLP
- Priority: FR 59843 2017.10.19
- Main IPC: F01D25/14
- IPC: F01D25/14 ; F01D25/12 ; F01D25/24

Abstract:
A distribution element intended to be fixed to a support structure for supplying cooling fluid to a wall to be cooled facing the distribution element, the distribution element including a body defining a cooling fluid distribution internal volume and a multi-perforated plate which delimits the internal volume and includes a plurality of outlet through-perforations which put the cooling fluid distribution internal volume into communication with the wall to be cooled, the distribution element including an inlet orifice opening into the cooling fluid distribution internal volume, wherein for directing the cooling fluid from the inlet orifice to the plurality of outlet through-perforations the cooling fluid distribution internal volume includes directional fins.
Public/Granted literature
- US20220412226A1 ELEMENT FOR DISTRIBUTING A COOLING FLUID AND ASSOCIATED TURBINE RING ASSEMBLY Public/Granted day:2022-12-29
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